CN109592061A - One kind being tethered at component - Google Patents
One kind being tethered at component Download PDFInfo
- Publication number
- CN109592061A CN109592061A CN201811340616.8A CN201811340616A CN109592061A CN 109592061 A CN109592061 A CN 109592061A CN 201811340616 A CN201811340616 A CN 201811340616A CN 109592061 A CN109592061 A CN 109592061A
- Authority
- CN
- China
- Prior art keywords
- hole
- tethered
- component
- rotary shaft
- pedestal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 26
- 238000007789 sealing Methods 0.000 claims description 8
- 229920003023 plastic Polymers 0.000 claims description 7
- 239000004033 plastic Substances 0.000 claims description 7
- 238000005452 bending Methods 0.000 description 2
- 238000010008 shearing Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
The application belongs to aircraft picketing fixed structure design field, in particular to one kind is tethered at component, comprising: pedestal 1 offers rotating hole for being fixedly connected with aircraft thereon；Rotary shaft 2, one end are arranged in rotating hole, and referred to as round end, the other end are known as upset end；Rotary shaft 2 can rotate in rotating hole；Mooring ring 5, outer ring and the upset end of rotary shaft 2 are hinged, and can overturn around tipping line；Wherein, tipping line is vertical with the axis of rotary shaft 2.
Description
Technical field
The application belongs to aircraft picketing fixed structure design field, in particular to one kind is tethered at component.
Background technique
To realize the fixation to aircraft on ground or warship face, multiple be tethered at generally is opened up in aircraft surfaces predetermined position and is connect
Mouthful, it component will be tethered at is fixed at and be tethered in interface, one end of cable wire is connect with the mooring ring being tethered on component, the other end
It is fixed on ground or warship face, is achieved in the fixation to aircraft on ground or warship face.
Currently, to aircraft be tethered at it is fixed used by be tethered in component, mooring ring only can in one direction into
The reciprocal flip-flop movement of row, when rope at different angles to aircraft picketing when, be tethered at the stress form of ring assemblies with different angles
Degree changes, it is made to be tethered at component when carrying out Intensity Design, to consider shearing under different angle, bending power, design
Journey is complicated, and the shearing for bearing multiple directions, bending power is used for multiple times to the unfavorable shadow of its service life generation in the component that is tethered at of the form
It rings.
Thus, it is desirable to have a kind of technical solution overcomes or at least mitigates at least one drawbacks described above of the prior art.
Summary of the invention
There is provided one kind to be tethered at component for the purpose of the application, the problem of to overcome or alleviated by above-mentioned at least one aspect.
The technical solution of the application is:
One kind being tethered at component, comprising:
Pedestal offers rotating hole for being fixedly connected with aircraft thereon；
Rotary shaft, one end are arranged in rotating hole, and referred to as round end, the other end are known as upset end；Rotary shaft can be
It is rotated in rotating hole；
The upset end of mooring ring, outer ring and rotary shaft is hinged, and can overturn around tipping line；Wherein,
Tipping line is vertical with the axis of rotary shaft.
Optionally, rotating hole is the step through-hole opened on the base, and step through-hole is divided into two sections, wherein one section is known as
Big hole section, the other end are known as aperture section, and big hole section diameter is greater than aperture section diameter；
Round end passes through aperture section, extends to big hole section, and be provided with caging bolt.
Optionally, aperture section is known as being connected to end towards big hole section one end；
Caging bolt is provided with limiting gasket with being connected between the end face of end.
Optionally, aperture section inner wall circumferentially offers seal groove, is provided with sealing ring in seal groove.
Optionally, plastics gasket circle is provided in seal groove, plastic washer is between sealing ring and rotary shaft.
Optionally, rotation axial wall plane is circumferentially arranged has limit to protrude, and limit protrusion is between pedestal and upset end.
Optionally, pedestal is circumferentially provided with pedestal protrusion along step through-hole towards a side surface of upset end, and pedestal is convex
It is protruded out with limit and contradicts connection.
Optionally, pedestal is a cylindrical body, and cylindrical outer surface offers external screw thread, and external screw thread with aircraft picketing for connecing
The screw-internal thread fit connection opened up in mouthful；
Step through-hole is along cylinder axis to opening up.
Optionally, multiple threaded holes are radially offered on cylindrical body, threaded hole by screw and aircraft picketing for connecing
Mouth is fixedly connected.
Optionally, upset end offers overturning through-hole along tipping line；
Mooring ring external annular surface is provided with two outer rings protrusion, and each outer ring protrusion is upper axially to be offered hingedly along overturning through-hole
Through-hole；
Upset end setting forms hinged channel between two hinged through-holes and overturning through-hole between two outer rings protrusion；
Link bolt is provided in hinged channel, link bolt and hinged nut are cooperatively connected；
Hinged nut and far ultraviolet ring convex are provided with hinged washer between going out；
Mooring ring can be rotated around link bolt.
At least there are following advantageous effects in the application: providing one kind and be tethered at component, wherein mooring ring is in addition to can
Outer around tipping line overturning, due also to coupled rotary shaft can rotate in rotating hole, mooring ring be can be realized at 360 degree
It is rotated in range around rotating shaft axis, be adapted to different angle is tethered at requirement, when being tethered to aircraft with any angle,
Mooring ring is able to rotate optimum fixation position, and stress is simple, is primarily subjected to the moment of flexure along rotary shaft axial force and vertical rotation axis,
And fixed angle is flexible, is tethered at conveniently.
Detailed description of the invention
Fig. 1 is the sectional view that the application is tethered at component；
Fig. 2 is the structural schematic diagram that the application is tethered at component.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application implementation clearer, below in conjunction in the embodiment of the present application
Attached drawing, technical solutions in the embodiments of the present application is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label indicate same or similar element or element with the same or similar functions.Described embodiment is the application
A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use
In explanation the application, and it should not be understood as the limitation to the application.Based on the embodiment in the application, ordinary skill people
Member's every other embodiment obtained without creative efforts, shall fall in the protection scope of this application.Under
Face is described in detail embodiments herein in conjunction with attached drawing.
In the description of the present application, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown is merely for convenience of description the application and simplifies description, rather than the dress of indication or suggestion meaning
It sets or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as protecting the application
The limitation of range.
1 to Fig. 2 the application is described in further details with reference to the accompanying drawing.
One kind being tethered at component, comprising:
Pedestal 1 offers rotating hole for being fixedly connected with aircraft thereon；
Rotary shaft 2, one end are arranged in rotating hole, and referred to as round end, the other end are known as upset end；Rotary shaft 2 can
It is rotated in rotating hole；
Mooring ring 5, outer ring and the upset end of rotary shaft 2 are hinged, and can overturn around tipping line；Wherein,
Tipping line is vertical with the axis of rotary shaft 2.
Further, rotating hole is the step through-hole opened on pedestal 1, and step through-hole is divided into two sections, wherein one section
Referred to as big hole section, the other end are known as aperture section, and big hole section diameter is greater than aperture section diameter；Round end passes through aperture section, extends to
Big hole section, and it is provided with caging bolt 10.
Further, aperture section is known as being connected to end towards big hole section one end；Caging bolt 10 is set with being connected between the end face of end
It is equipped with limiting gasket 9.
Further, aperture section inner wall circumferentially offers seal groove, and sealing ring 8 is provided in seal groove.
Further, plastics gasket circle 7 is provided in seal groove, plastic washer 7 is between sealing ring 8 and rotary shaft 2.
Sealing ring 8 and plastic washer 7 are equipped in seal groove, and the foreign matters such as sand and dust, rainwater can be prevented along rotary shaft 2
Gap between rotating hole enters the inside of pedestal 1, avoids thus damaging the verticity of rotary shaft 2 or to internal junction
It is configured to corrode.
Further, 2 wall surface of rotary shaft is circumferentially arranged has limit to protrude, limit protrusion be located at pedestal 1 and upset end it
Between.
Limit protrusion is equipped with caging bolt can limit rotary shaft 2 along axial movement, make to be tethered between modular construction
Stablize, and interstructural abrasion can be reduced, prolongs its service life.
Further, pedestal 1 is circumferentially provided with pedestal protrusion, pedestal along step through-hole towards a side surface of upset end
Protrusion contradicts connection with limit protrusion.
Further, pedestal 1 is a cylindrical body, and cylindrical outer surface offers external screw thread, and external screw thread is used for and aircraft system
The screw-internal thread fit opened up in interface is stayed to connect；Step through-hole is along cylinder axis to opening up.
Further, multiple threaded holes are radially offered on cylindrical body, threaded hole is used to pass through screw and aircraft picketing
Interface is fixedly connected.
Further, upset end offers overturning through-hole along tipping line；5 external annular surface of mooring ring is provided with two outer ring convex
Out, each outer ring protrusion is upper axially offers hinged through-hole along overturning through-hole；Upset end setting is between two outer rings protrusion, two hinges
It connects between hole and overturning through-hole and forms hinged channel；Link bolt 3, link bolt 3 and hinged spiral shell are provided in hinged channel
Mother is cooperatively connected；Hinged nut and far ultraviolet ring convex are provided with hinged washer 4 between going out；Mooring ring 5 can be 3 turns around link bolt
It is dynamic.
The above, the only specific embodiment of the application, but the protection scope of the application is not limited thereto, it is any
Within the technical scope of the present application, any changes or substitutions that can be easily thought of by those familiar with the art, all answers
Cover within the scope of protection of this application.Therefore, the protection scope of the application should be with the scope of protection of the claims
It is quasi-.
Claims (10)
1. one kind is tethered at component characterized by comprising
Pedestal (1) offers rotating hole for being fixedly connected with aircraft thereon；
Rotary shaft (2), one end are arranged in the rotating hole, and referred to as round end, the other end are known as upset end；The rotary shaft
(2) it can be rotated in the rotating hole；
Mooring ring (5), outer ring and the upset end of the rotary shaft (2) are hinged, and can overturn around tipping line；Wherein,
The tipping line is vertical with the axis of the rotary shaft (2).
2. according to claim 1 be tethered at component, which is characterized in that
The rotating hole is the step through-hole opened on the pedestal (1), and the step through-hole is divided into two sections, wherein one section
Referred to as big hole section, the other end are known as aperture section, and the big hole section diameter is greater than the aperture section diameter；
The round end passes through the aperture section, extends to the big hole section, and be provided with caging bolt (10).
3. according to claim 2 be tethered at component, which is characterized in that
The aperture section is known as being connected to end towards described big hole section one end；
The caging bolt (10) is provided with limiting gasket (9) with described be connected between the end face of end.
4. according to claim 2 be tethered at component, which is characterized in that the aperture section inner wall circumferentially offers sealing
Slot is provided with sealing ring (8) in the seal groove.
5. volume according to claim 4 is tethered at component, which is characterized in that be provided with plastics gasket circle in the seal groove
(7), the plastic washer (7) is between the sealing ring (8) and the rotary shaft (2).
6. according to claim 2 be tethered at component, which is characterized in that rotary shaft (2) wall surface is circumferentially arranged limited
Position protrusion, the limit protrusion is between the pedestal (1) and the upset end.
7. according to claim 6 be tethered at component, which is characterized in that the pedestal (1) is towards the side of the upset end
Surface is circumferentially provided with pedestal protrusion along the step through-hole, and the pedestal protrusion contradicts connection with limit protrusion.
8. according to claim 2 be tethered at component, which is characterized in that
The pedestal (1) is a cylindrical body, and the cylindrical outer surface offers external screw thread, and the external screw thread is used to fly with described
Machine is tethered at the screw-internal thread fit connection opened up in interface；
The step through-hole is along the cylinder axis to opening up.
9. according to claim 8 be tethered at component, which is characterized in that radially offer multiple screw threads on the cylindrical body
Hole, the threaded hole by screw with the aircraft picketing interface for being fixedly connected.
10. according to claim 1 be tethered at component, which is characterized in that
The upset end offers overturning through-hole along the tipping line；
Mooring ring (5) external annular surface is provided with two outer rings protrusion, and each outer ring is protruded along the overturning through-hole axis
To offering hinged through-hole；
The upset end setting forms hinge between the two outer ring protrusions between the two hinged through-holes and the overturning through-hole
Connect road；
It is provided in the hinged channel link bolt (3), the link bolt (3) and hinged nut are cooperatively connected；
Hinged washer (4) are provided between the hinged nut and the remote outer ring protrusion；
The mooring ring (5) can rotate around the link bolt (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811340616.8A CN109592061A (en) | 2018-11-12 | 2018-11-12 | One kind being tethered at component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811340616.8A CN109592061A (en) | 2018-11-12 | 2018-11-12 | One kind being tethered at component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109592061A true CN109592061A (en) | 2019-04-09 |
Family
ID=65957645
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811340616.8A Pending CN109592061A (en) | 2018-11-12 | 2018-11-12 | One kind being tethered at component |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109592061A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109533366A (en) * | 2018-11-13 | 2019-03-29 | 中国直升机设计研究所 | A kind of double freedom mooring device and its design method |
| CN113848083A (en) * | 2021-12-01 | 2021-12-28 | 中国飞机强度研究所 | Freezing and thawing prevention terrace for airplane test and freezing and thawing prevention parameter optimization method |
| CN115051308A (en) * | 2022-07-04 | 2022-09-13 | 深圳市亮视智能工程有限公司 | Unmanned aerial vehicle wire loop structure, mobile power supply box and lamp switching control method thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201907634U (en) * | 2010-10-27 | 2011-07-27 | 上海海洋大学 | U-shaped submerged buoy mooring device |
| CN203111505U (en) * | 2013-01-29 | 2013-08-07 | 中国航空工业集团公司西安飞机设计研究所 | Rapid mooring device used for airplane floor |
| CN105980252A (en) * | 2013-12-10 | 2016-09-28 | 谷歌公司 | Systems and apparatus for tether termination mount for tethered aerial vehicles |
| CN206734652U (en) * | 2017-04-24 | 2017-12-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft picketing structure |
| CN206841701U (en) * | 2017-05-04 | 2018-01-05 | 中国特种飞行器研究所 | Tether cable system and sightseeing captive balloon |
| CN207417069U (en) * | 2017-11-10 | 2018-05-29 | 中船黄埔文冲船舶有限公司 | Mooring device |
-
2018
- 2018-11-12 CN CN201811340616.8A patent/CN109592061A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201907634U (en) * | 2010-10-27 | 2011-07-27 | 上海海洋大学 | U-shaped submerged buoy mooring device |
| CN203111505U (en) * | 2013-01-29 | 2013-08-07 | 中国航空工业集团公司西安飞机设计研究所 | Rapid mooring device used for airplane floor |
| CN105980252A (en) * | 2013-12-10 | 2016-09-28 | 谷歌公司 | Systems and apparatus for tether termination mount for tethered aerial vehicles |
| CN206734652U (en) * | 2017-04-24 | 2017-12-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft picketing structure |
| CN206841701U (en) * | 2017-05-04 | 2018-01-05 | 中国特种飞行器研究所 | Tether cable system and sightseeing captive balloon |
| CN207417069U (en) * | 2017-11-10 | 2018-05-29 | 中船黄埔文冲船舶有限公司 | Mooring device |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109533366A (en) * | 2018-11-13 | 2019-03-29 | 中国直升机设计研究所 | A kind of double freedom mooring device and its design method |
| CN113848083A (en) * | 2021-12-01 | 2021-12-28 | 中国飞机强度研究所 | Freezing and thawing prevention terrace for airplane test and freezing and thawing prevention parameter optimization method |
| CN113848083B (en) * | 2021-12-01 | 2022-02-18 | 中国飞机强度研究所 | Freezing and thawing prevention terrace for airplane test and freezing and thawing prevention parameter optimization method |
| CN115051308A (en) * | 2022-07-04 | 2022-09-13 | 深圳市亮视智能工程有限公司 | Unmanned aerial vehicle wire loop structure, mobile power supply box and lamp switching control method thereof |
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Legal Events
| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190409 |